[0001] This invention relates to high speed optical scanners. More particularly, this invention
relates to high speed optical scanners for use with finite conjugates and visible
light.
[0002] A basic compact video rate optical scanner (CVROS) system is described in detail
in US-A-4,538,181 and is shown in Fig. 11. The disclosure of this patent is incorporated
herein in its entirety by reference. In this system, incoming radiation from an image
is reflected off a framing mirror 20 through a meniscus lens 22, past a strip mirror
24 to an objective mirror 26. The radiation is then focused on strip mirror 24 and
reflected toward the concave reflectors 28 of rotating scan disc 30, from which it
emerges as a collimated beam. The collimated beam passes the strip mirror and is focused
on detector 32 by means of a collector reflector 34. A two dimensional raster scan
my be obtained by oscillating framing mirror 20 located at the aperture stop and synchronized
to the scan disc.
[0003] The curved strip mirror 24 is the exterior surface of a cone formed with a 45 degree
half-angle and an axis which is coaxial with the axis of rotation for scan disc 30
as indicated by dotted lines 36. Objective mirror 26 is a concave mirror with a spherical
contour having a radius equal to the distance from the vertex of framing mirror 20.
The reflected image off objective mirror 26 lies on a spherical surface which is intercepted
by curved strip mirror 24. The radius of curvature of the image is one-half the radius
of curvature of objective mirror 26 and is equal to the scan disk radius R
d.
[0004] The CVROS scanner described in US-A-4,538,181, however, suffers from significant
limitations preventing its utilization in applications with finite conjugates and
visible light. The CVROS scanner was originally developed for infrared applications.
Consequently, all lens materials were made from material which transmits infrared
radiation but not visible light, and are therefore inappropriate for applications
in the visual spectrum.
[0005] For example, adaptation of the CVROS scanner for applications in the visible, ultra-violet
or near infrared spectrums requires elimination of the germanium meniscus lens because
of its spectral transmission limitations. This results in the need for a meniscus
lens of a different material for the spectrum of interest, or to correct the spherical
aberration by another means. A single lens is suitable only for essentially monochromatic
applications, Broad spectral band applications would require and achromatic corrector
lens which can correct chromatic aberration both on--axis and off-axis.
[0006] On-axis aberrations of the scanner are those which occur when the scan disc concave
reflector is centered on the optical axis. Off-axis aberrations of the scanner are
those which arise during the repositioning of the scan disc concave reflector as it
rotates about the scan disc axis. With a perfectly symmetrical, monocentric system
which includes the concentric curved image surface, the off-axis aberrations are identical
to the on-axis aberrations, Thus, with respect to the off-axis imagery for applications
which require a flat image, the well-corrected curved image must be transformed into
a flat image while maintaining the high degree of correction present across the entire
arc length of the curved image.
[0007] Adaptation of the scanner to finite conjugate applications also requires dealing
with the field curvature problem which arises. As is illustrated in Fig. 12, the image
surface 38 (or object surface depending on application) for which the scanner retains
its concentric form is spherical. In Fig. 12, Rm designates the objective mirror radius,
Rs the strip mirror radius, and Ri the radius of the image. The image and object conjugates
of the objective mirror are designated S' and S, respectively. For many applications,
it is required that the scanner image onto a flat surface. Further, for applications
in which the imaging medium or art work are located on a rotating drum or flat bed
transport, the scanner need only produce a flat line scan and not a flat two-dimensional
area scan.
SUMMARY OF THE INVENTION
[0008] With the foregoing in mind, it is an object of the invention to provide a high speed
optical scanner for use with finite conjugates and visible light.
[0009] In accordance with the invention, an optical system comprises a rotating scan disc
including a circular array of concave reflectors on a planar surface thereof; imaging
means adapted to coincide with the scanning sweep of the concave reflectors and separated
from said concave reflectors by a distance equal to the focal length of said concave
reflectors; and a light source positioned to emit light toward said circular array
of concave reflectors to form an image redirected from said imaging means; wherein
said imaging means includes means adapted to correct field curvature of said image.
[0010] In accordance with the invention, a non-concentric objective mirror and a strip prism
replacing the strip mirror are provided to achieve field flatness in high speed optical
scanners. The coma exhibited by the non-concentric objective mirror and the strip
prism are approximately equal in magnitude but opposite in sign and an optimum combination
of non-concentric objective mirror radius and strip mirror cylinder radius may be
chosen for different system magnifications. The resulting image remains well corrected
for field curvature and is essentially free of coma.
[0011] Compensation for scan disc axis tilt or decenter via beam position monitoring in
the scan direction can be achieved by providing a beam splitter and precision grating
located parfocal to the strip mirror. As the beam traverses the precision grating,
a clocking signal is generated which is characteristic of the system with all of its
perturbations and which can be used to time the system electronic events in lieu of
a fixed frequency clock. This beam position monitoring design can be extended to the
cross-scan direction by utilizing two or more slightly non-parallel light beams generated,
e.g., by two pin holes and a collimating mirror.
[0012] Sinusoidal cross-scan displacement errors due to disc axis tilt and decenter can
also be eliminated by repositioning the beam at the same frequency and amplitude and
with the correct phase relationship. The light beam may be repositioned by movement
of an optical component, e.g., the strip mirror. The light beam can also be repositioned
by changing its angle of incidence on the scan disc via a tipped plate located between
a laser diode and a collimating lens.
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] The accompanying drawings illustrate preferred embodiments of the invention and,
together with the description, serve to explain the principles of the invention.
[0014] Fig. 1 shows a strip prism field flattener design in accordance with the invention.
[0015] Fig. 2 shows an image plane chief rays for the strip prism design.
[0016] Fig. 3 shows strip prism transverse ray aberrations.
[0017] Fig. 4 shows a beam position monitoring system in accordance with the invention.
[0018] Fig. 5 shows a reticle pattern and resulting clock signal for beam position monitoring
in the scan direction.
[0019] Fig. 6 shows a horizontal and vertical scan position monitor.
[0020] Fig. 7 shows output signals for a three pattern reticle.
[0021] Fig. 8 shows reticle patterns and resulting clock signals for beam position monitoring
in the cross-scan direction.
[0022] Fig. 9 shows a CVROS scanner with voice coils for movement on the strip mirror.
[0023] Fig. 10 shows the dithering of the strip mirror to accommodate decentering of the
scan disc.
[0024] Fig. 11 shows a basic compact video rate optical scanner (CVROS).
[0025] Fig. 12 shows the image surface associated with the CVROS scanner of Fig. 11.
DETAILED DESCRIPTION OF THE DRAWINGS
[0026] In accordance with the invention, two related designs to achieve field flatness in
high speed optical scanners are presented: 1) a non-concentric objective mirror, and
2) a strip prism field flattener which replaces the strip mirror. These designs may
be utilized separately or, as in a preferred embodiment, in combination.
[0027] The non-concentric objective mirror design to achieve field flattening provides that
the image conjugate for an off-axis field point be lengthened by a slight increase
in magnification for that point such that the image is formed on the tangent plane
to the curved image instead of being formed on the curved image surface itself. The
magnification increase is achieved by locating an objective mirror 26 of radius shorter
than the basic CVROS scanner design, non-concentrically to the strip mirror 24 (Fig.
11). This results in a reduction in the length of the object conjugate for points
off-axis, a reduction which increases progressively as the distance off-axis increases.
The assumed object is the arc on the strip mirror defined by the intersection of the
concave reflector focal point as it rotates across the strip mirror. While this design
achieves field flatness beyond 60 degrees, it exhibits coma which progresses steadily
in magnitude as the distance off-axis is increased.
[0028] In the strip prism field flattener design, the strip mirror 24 (Fig. 11) is replaced
by a strip prism 102 (Fig. 1) which retains the same conical reflecting surface as
the strip mirror, but which, in cross-section, resembles a 1.5 mm right angle (45°
-45° -90°) prism. The entrance face 104 is plano, and is parallel to the plane of
the scan disc. Reflective surface 106 is conical. The exit surface 108 of the prism
is cylindrical, with the radius of curvature (Rp) of the exit surface being non-concentric
with and substantially longer than the radius of curvature (Rs) of the reflective
surface 106 of the prism so as to create a negative field flattening lens.
[0029] The introduction of this refractive component results in a small amount of axial
chromatic aberration, λ/4 or less, across the visible spectrum. More importantly,
no lateral chromatic aberration exists. The strip prism also has the advantage that
no large field mirror is required and its scan characteristic approximates F tan ϑ
rather than F ϑ. However, while the strip prism arrangement achieves a high degree
of field flattening, it also exhibits coma.
[0030] Advantageously, the coma exhibited by the non-concentric objective mirror and the
strip prism are approximately equal in magnitude but opposite in sign and an optimum
combination of non-concentric objective mirror radius and strip mirror cylinder radius
has been found to exist for different system magnifications. The resulting image remains
well corrected for field curvature, but is now essentially free of the coma which
exists in designs that may rely on either the non-concentric objective mirror or strip
prism alone.
[0031] The image plane chief rays for the strip prism design are illustrated in Fig. 2 for
ϑ = 0° to 30°. As illustrated, X = 262.1 mm, Y = 0.0 mm, ϑ = 31.9°, and

. The strip prism residual transverse ray aberrations are shown in Fig. 3.
[0032] An evaluation of the strip prism design indicates that the correction at 587 nanometers
is λ/10 or better for semi-fields out to 22.5°, but falls to λ/4 at 30° semi-field.
The strip prism introduces a relatively small amount of primary axial and lateral
chromatic aberration. On-axis there is a λ/4 focus difference between 587 and 486
nanometers. At 22.5° semi-field there is a 6 micrometers lateral spread between the
focal points for 656 and 486 nanometers. This increases to 10 micrometers at 30° semi-field,
about one-half the airy disc diameter. The location of the image point along the scan
line, as measured from the center of the field, follows the tangent function of the
scan disc rotation angle to within 1% out to a semi-line length of 262 mm.
[0033] It may be appreciated that the location of the beam in the scan direction at any
instant during the line scan will depart from its ideal location of there is any scan
disc axis tilt or decenter. Other potential sources of this error include hearing
jitter, motor cogging, angle position encoder error and drive electronics servo errors.
The combined effects of all of these sources of error result in a horizontal scan
function which is non-linear and which exhibits both systematic and random components.
[0034] In some systems, the magnitude of the combined effects may be small enough to not
require compensation. There compensation is required, however, beam position monitoring
can be achieved via implementation of a beam splitter and precision grating located
parfocal to the strip mirror as shown in Fig. 4. Preferably, a thin beam splitter
plate 112 is located between strip mirror 24 and scan disc 30. A beam of collimated
light is generated via pinhole 114, light source 116 and collimated mirror 118. The
collimated light passes through beam splitter plate 112 and strikes scan disc 30 at
normal incidence. The light reflected from the concave reflector 28 and beam splitter
plate 112 is focused onto precision grating 120, collected by field lens 122 and transmitted
to detector 124. Precision grating 120 is curved, having a radius equal to the scan
disc radius, and its arc length equals that of the strip mirror. As the beam traverses
the grating a clocking signal is generated which is characteristic of the system with
all of its perturbations and which can be used to time the system electronic events
in lieu of a fixed frequency clock.
[0035] As illustrated in Fig. 5, a reticle pattern 126 provided in precision grating 120
for beam position monitoring in the scan direction will allow the scanning light spot
to generate a signature system clock signal 128. Advantageously, by incorporating
a suitable reticle for beam position monitoring in the scan direction and generating
a clock signal which embodies all characteristics of the system, it is not necessary
to incorporate special F ϑ lenses.
[0036] The beam position monitoring design illustrated in Fig. 4 can be extended to include
beam position monitoring in the cross-scan direction. In this embodiment, two slightly
non-parallel light beams are generated by two slits or pin holes. The horizontal position
slit is oriented vertically and the vertical position slit is tilted at an angle as
shown in Fig. 6. Slits have the advantage, when compared with pin holes, of producing
greater illumination and, therefore, greater signal strength on the detectors. This
yields greater position accuracy when measuring threshold crossings of the detected
waveform. The two beams are focused onto corresponding reticles as shown in Fig. 6.
The placement of the slits yields two beams which are displaced from one another on
the reticle. The upper reticle pattern is identical to the one previously described
for measuring horizontal position. The lower reticle pattern consists of slits tilted
at the same angle as the source slit. Light from both beams is focused by a field
lens and sent to separate detectors.
[0037] Separation of the two beams can be accomplished in one of several ways. The two beams
are displaced from each other where they come to focus at the reticle. A fold mirror
located just behind the reticle can be used to intercept one of the beams after it
has passed through the reticle and send it to a separate field lens/detector combination.
Alternatively, the two beams can be distinguished from one another by locating color
filters in front of the slits (pin holes), e.g., red and green. After the two beams
pass through the reticle and field lens, a dichroic beam splitter is used to separate
the beams for detection.
[0038] If there is no cross-scan position error present, the output signals from the two
detector channels are in phase. When a cross-scan error is present, the slit patterns
shift together vertically on the reticle. This results in a phase shift of the clock
signal 125 from the horizontal detector channel relative to the clock signal 127 from
the vertical detector channel as shown in Fig. 6. The phase shift is proportional
to the vertical displacement error of the optical beam.
[0039] If the vertical displacement error is large enough, a 360 phase shift will be produced
resulting in a vertical position ambiguity. This ambiguity can be resolved by adding
a third pattern to the reticle. This pattern consists of wider slits at wider spacing.
This allows a larger error to be sensed as shown in Fig. 7. First vertical position
clock signal 129 and second vertical position clock signal 131 provide a maximum unambiguous
position error E. Thus, the maximum unambiguous position error may be increased by
employing a reticle having multiple patterns.
[0040] Fig. 8 is an alternative reticle pattern which also can provide vertical position
monitoring. If there is no cross-scan position error present, the output signals from
the red and green detectors are identical constant frequency clock signals 132. When
a cross-scan error is present, the red and green light spots at the detectors shift
together radially on the reticle. The resultant clock signals generated by the detectors
change and differ from one another, as shown on the right in Fig. 8. The time average
difference 134 between the two clock signals is proportional to the cross-scan error.
Advantageously, either of the two signals can also be used to simultaneously monitor
the beam position in the scan direction.
[0041] The error in the cross-scan beam position sensed by the beam position monitor can
be used to correct the beam's position line-by-line, pixel-by-pixel or at some intermediate
rate. The actual sampling rate will depend on system accuracy requirements, the size
and number of pixies per line, and line scan rate requirements.
[0042] The sinusoidal cross-scan displacement errors due to disc axis tilt and decenter
can also be eliminated by repositioning the beam at the same frequency and amplitude
and with the correct phase relationship. This can be achieved on a line-by-line basis
using beam position information gathered once per line. Errors which occur at a rate
higher than the line rate can be similarly corrected via multiple samples of the beam
position during a line scan.
[0043] An open loop approach in which the beam position is used only at assembly to set
the amplitude and phase of the beam positioner and is not part of the scanner is a
viable, lower cost approach when the error is chiefly sinusoidal and occurring at
the scan disc rotation frequency. This permits a relatively low frequency correction
technique to be implemented.
[0044] There are several ways to reposition the light beam which are known in the art, most
of them involving the movement of an optical component. In accordance with the preferred
embodiment herein, the strip mirror is the optical component. Since the line correction
rate can be of the order of several thousands times per second, a smaller and lighter
component such as the strip mirror is preferable to a larger and heavier one.
[0045] Figs. 9 and 10 illustrate beam positioning by movement of the strip mirror. In Fig.
9, scan disc 30 is shown rotating about axis of rotation 110 at a frequency of and
having optical axis 136. Two voice coils, 138, 140 provided with a drive voltage v
= v sine t are connected to strip mirror 24. By translating the strip mirror vertically
in synchronization with the moving light spot located at the focal point of the concave
reflector 28, the cross-scan error can be eliminated. As shown in Figs. 9 and 10 for
the case of scan disc decenter, the focused light spot oscillates along a radial line
136. If the optical axis of the concave reflector 28, on which the concave reflector
focal point is located, always intersects the strip mirror at the point of intersection
with the objective mirror axis, cross-scan error will be nulled.
[0046] In Fig. 10, the decentered position of the scan disc is illustrated by dashed lines
142. The true position of the light beam is shown at 144 and the decentered position
at 146. The dithered position of the strip mirror for line wobble correction is shown
at dashed line 148. In the case of scan disc axis tilt, there is a residual focus
error of amplitude z = (r-f) O. By making the concave reflector focal length f equal
to the scan disc radius R
D, the focus error can also be eliminated.
[0047] The strip mirror can be driven by various means. Voice coils or a piezoelectric drive
are suitable since the required displacement amplitude is typically of the order of
10 micrometers or less. Voice coils have been successfully utilized where the required
displacement amplitude of the strip mirror was +4 micrometers. A satisfactory approximation
to translating the strip mirror can also be achieved by flexing it about a horizontal
axis. The distance between the strip mirror and its tilt axis can be equal to the
scan disc radius and yield satisfactory results for a 30 degree field.
[0048] The light beam can also be repositioned by changing its angle of incidence on the
scan disc. This can be accomplished via a tipped plate located between a laser diode
and a collimating lens. A tipped plate located in a converging or diverging beam displaces
the virtual image of the laser point source in proportion to the plate thickness and
tip angle. This, in turn, changes the angle of incidence at which the collimated light
strikes the concave reflector of the scan disc and thereby effects a radial shift
in the concave reflector focal point location at the strip mirror.
[0049] By dithering the plate tip angle in proportion to the output from the cross-scan
beam position sensor, the beam position error can be nulled continuously through implementation
of a servo system. By providing the means to tip the plate in the orthogonal direction,
beam direction changes in the scan direction can also be effected.
[0050] The tipped plates relative insensitivity of displacement versus angle of tilt can
be a useful property when small displacements of the order of 10 micrometers are required.
Also, being located near a point source object it can be very small, thereby allowing
it to be dithered at high frequency.
[0051] Other means of repositioning the beam external to the scanner are also possible.
For example, the laser diode itself can be mounted on a piezoelectric block and translated
directly, or a small, dithered fold mirror can be used in front of the diode to yield
a satisfactory approximation to translation of the laser source. Techniques employed
for other scanners may also be viable.
[0052] Changes may also be made within the purview of the appended claims without departing
from the scope and spirit of the invention. For example, while beam position monitoring
was described with a beam splitter and a precision grating located parfocal to the
strip mirror, the precision grating can also be located parfocal to the scan line
and extending over its length.
1. An optical system, comprising:
a rotating scan disc (30) including a circular array of concave reflectors (28)
on a planar surface thereof;
imaging means adapted to coincide with the scanning sweep of the concave reflectors
(28) and separated from said concave reflectors by a distance equal to the focal length
of said concave reflectors; and
a light source (116, Fig. 4) positioned to emit light toward said circular array
of concave reflectors (28) to form an image redirected from said imaging means;
wherein said imaging means includes means adapted to correct field curvature of
said image.
2. The optical system of claim 1, wherein said means adapted to correct field curvature
of said image includes a non-concentrically positioned strip mirror (24) and objective
mirror (26).
3. The optical system of claim 1, wherein said imaging means includes a strip prism (102).
4. The optical system of claim 3, wherein said imaging means includes an objective mirror
(26).
5. The optical system of claim 2 or 4, wherein the objective mirror image conjugate to
an off-axis field point is lengthened such that the image is formed on the tangent
plane to the uncorrected image instead of being formed on the uncorrected image surface
itself.
6. The optical system of claim 3 or 5, wherein said strip prism (102) has a right triangular
cross section with a plano entrance (104) , a conical reflective surface (104), and
a cylindrical exit surface (108).
7. The optical system of claim 6, wherein the exit surface (108) of said strip prism
(102) is cylindrical, with the radius Rp of the exit surface of the prism being non-concentric with and longer than the radius
Rs of the reflective surface (106) of the prism (102).
8. The optical system of claim 1, further comprising means for monitoring the position
of said light beam during rotation of said scan disc (30).
9. The optical system of claim 8, wherein said means for monitoring further comprises
a beam splitter (112, Fig. 4) and a grating (120).
10. The optical system of claim 9, wherein said grating (120) includes a reticle pattern
(126, Fig. 5) for generating a clock signal (128) representing characteristics of
the system.
11. The optical system of claim 8, wherein said means for monitoring further comprises
two non-parallel light beams utilized to monitor beam position in both the scan and
cross-scan directions.
12. The optical system of claim 10, wherein said imaging means includes an objective mirror
(26) and a strip prism (102) adapted to correct field curvature of said image.
13. The optical system of claim 2, further comprising means for moving at least one optical
component of said imaging means to reposition said light beam.
14. The optical system of claim 13, wherein said at least one optical component is a strip
mirror (24).
15. The optical system of claim 13, wherein said means for moving includes at least one
voice coil (138 Fig. 9).
16. The optical system of claim 13, wherein said at least one optical component is a tipped
plate.
17. The optical system of claim 13, further comprising means for monitoring the position
of said light beam during rotation of said scan
18. The optical system of claim 13, wherein said imaging means includes an objective mirror
(26) and a strip prism (102) adapted to correct field curvature of said image.